Helicopter

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COPYRIGHT 1996 Gale Research Inc.

Helicopter

Background

Helicopters are classified as rotary wing aircraft, and their rotary wing is commonly referred to as the main rotor or simply the rotor. Unlike the more common fixed wing aircraft such as a sport biplane or an airliner, the helicopter is capable of direct vertical take-off and landing; it can also hover in a fixed position. These features render it ideal for use where space is limited or where the ability to hover over a precise area is necessary. Currently, helicopters are used to dust crops, apply pesticide, access remote areas for environmental work, deliver supplies to workers on remote maritime oil rigs, take photographs, film movies, rescue people trapped in inaccessible spots, transport accident victims, and put out fires. Moreover, they have numerous intelligence and military applications.

Numerous individuals have contributed to the conception and development of the helicopter. The idea appears to have been bionic in origin, meaning that it derived from an attempt to adapt a natural phenomena—in this case, the whirling, bifurcated fruit of the maple tree—to a mechanical design. Early efforts to imitate maple pods produced the whirligig, a children's toy popular in China as well as in medieval Europe. During the fifteenth century, Leonardo da Vinci, the renowned Italian painter, sculptor, architect, and engineer, sketched a flying machine that may have been based on the whirligig. The next surviving sketch of a helicopter dates from the early nineteenth century, when British scientist Sir George Cayley drew a twin-rotor aircraft in his notebook. During the early twentieth century, Frenchman Paul Cornu managed to lift himself off the ground for a few seconds in an early helicopter. However, Cornu was constrained by the same problems that would continue to plague all early designers for several decades: no one had yet devised an engine that could generate enough vertical thrust to lift both the helicopter and any significant load (including passengers) off the ground.

Igor Sikorsky, a Russian engineer, built his first helicopter in 1909. When neither this prototype nor its 1910 successor succeeded, Sikorsky decided that he could not build a helicopter without more sophisticated materials and money, so he transferred his attention to aircraft. During World War I, Hungarian engineer Theodore von Karman constructed a helicopter that, when tethered, was able to hover for extended periods. Several years later, Spaniard Juan de la Cierva developed a machine he called an autogiro in response to the tendency of conventional airplanes to lose engine power and crash while landing. If he could design an aircraft in which lift and thrust (forward speed) were separate functions, Cierva speculated, he could circumvent this problem. The autogiro he subsequently invented incorporated features of both the helicopter and the airplane, although it resembled the latter more. The autogiro had a rotor that functioned something like a windmill. Once set in motion by taxiing on the ground, the rotor could generate supplemental lift; however, the autogiro was powered primarily by a conventional airplane engine. To avoid landing problems, the engine could be disconnected and the autogiro brought gently to rest by the rotor, which would gradually cease spinning as the machine reached the ground. Popular during the 1920s and 1930s, autogiros ceased to be produced after the refinement of the conventional helicopter.

The helicopter was eventually perfected by Igor Sikorsky. Advances in aerodynamic theory and building materials had been made since Sikorsky's initial endeavor, and, in 1939, he lifted off the ground in his first operational helicopter. Two years later, an improved design enabled him to remain aloft for an hour and a half, setting a world record for sustained helicopter flight.

The helicopter was put to military use almost immediately after its introduction. While it was not utilized extensively during World War II, the jungle terrain of both Korea and Vietnam prompted the helicopter's widespread use during both of those wars, and technological refinements made it a valuable tool during the Persian Gulf War as well. In recent years, however, private industry has probably accounted for the greatest increase in helicopter use, as many companies have begun to transport their executives via helicopter. In addition, helicopter shuttle services have proliferated, particularly along the urban corridor of the American Northeast. Still, among civilians the helicopter remains best known for its medical, rescue, and relief uses.

Design

A helicopter's power comes from either a piston engine or a gas turbine (recently, the latter has predominated), which moves the rotor shaft, causing the rotor to turn. While a standard plane generates thrust by pushing air behind its wing as it moves forward, the helicopter's rotor achieves lift by pushing the air beneath it downward as it spins. Lift is proportional to the change in the air's momentum (its mass times its velocity): the greater the momentum, the greater the lift.

Helicopter rotor systems consist of between two and six blades attached to a central hub. Usually long and narrow, the blades turn relatively slowly, because this minimizes the amount of power necessary to achieve and maintain lift, and also because it makes controlling the vehicle easier. While light-weight, general-purpose helicopters often have a two-bladed main rotor, heavier craft may use a four-blade design or two separate main rotors to accommodate heavy loads.

To steer a helicopter, the pilot must adjust the pitch of the blades, which can be set three ways. In the collective system, the pitch of all the blades attached to the rotor is identical; in the cyclic system, the pitch of each blade is designed to fluctuate as the rotor revolves, and the third system uses a combination of the first two. To move the helicopter in any direction, the pilot moves the lever that adjusts collective pitch and/or the stick that adjusts cyclic pitch; it may also be necessary to increase or reduce speed.

Unlike airplanes, which are designed to minimize bulk and protuberances that would weigh the craft down and impede airflow around it, helicopters have unavoidably high drag. Thus, designers have not utilized the sort of retractable landing gear familiar to people who have watched planes taking off or landing—the aerodynamic gains of such a system would be proportionally insignificant for a helicopter. In general, helicopter landing gear is much simpler than that of airplanes. Whereas the latter require long runways on which to reduce forward velocity, helicopters have to reduce only vertical lift, which they can do by hovering prior to landing. Thus, they don't even require shock absorbers: their landing gear usually comprises only wheels or skids, or both.

One problem associated with helicopter rotor blades occurs because airflow along the length of each blade differs widely. This means that lift and drag fluctuate for each blade throughout the rotational cycle, thereby exerting an unsteadying influence upon the helicopter. A related problem occurs because, as the helicopter moves forward, the lift beneath the blades that enter the airstream first is high, but that beneath the blades on the opposite side of the rotor is low. The net effect of these problems is to destabilize the helicopter. Typically, the means of compensating for these unpredictable variations in lift and drag is to manufacture flexible blades connected to the rotor by a hinge. This design allows each blade to shift up or down, adjusting to changes in lift and drag.

Torque, another problem associated with the physics of a rotating wing, causes the helicopter fuselage (cabin) to rotate in the opposite direction from the rotor, especially when the helicopter is moving at low speeds or hovering. To offset this reaction, many helicopters
use a tail rotor, an exposed blade or ducted fan mounted on the end of the tail boom typically seen on these craft. Another means of counteracting torque entails installing two rotors, attached to the same engine but rotating in opposite directions, while a third, more space-efficient design features twin rotors that are enmeshed, something like an egg beater. Additional alternatives have been researched, and at least one NOTAR (no tail rotor) design has been introduced.

Raw Materials

The airframe, or fundamental structure, of a helicopter can be made of either metal or organic composite materials, or some combination of the two. Higher performance requirements will incline the designer to favor composites with higher strength-to-weight ratio, often epoxy (a resin) reinforced with glass, aramid (a strong, flexible nylon fiber), or carbon fiber. Typically, a composite component consists of many layers of fiber-impregnated resins, bonded to form a smooth panel. Tubular and sheet metal substructures are usually made of aluminum, though stainless steel or titanium are sometimes used in areas subject to higher stress or heat. To facilitate bending during the manufacturing process, the structural tubing is often filled with molten sodium silicate. A helicopter's rotary wing blades are usually made of fiber-reinforced resin, which may be adhesively bonded with an external sheet metal layer to protect edges. The helicopter's windscreen and windows are formed of polycarbonate sheeting.

The ManufacturingProcess

In 1939, a Russian emigre to the United States tested what was to become a prominent prototype for later helicopters. Already a prosperous aircraft manufacturer in his native land, Igor Sikorsky fled the 1917 revolution, drawn to the United States by stories of Thomas Edison and Henry Ford.

Sikorsky soon became a successful aircraft manufacturer in his adopted homeland. But his dream was vertical take-off, rotary wing flight. He experimented for more than twenty years and finally, in 1939, flew his first flight in a craft dubbed the VS 300. Tethered to the ground with long ropes, his craft flew no higher than 50 feet off the ground on its first several flights. Even then, there were problems: the craft flew up, down, and sideways, but not forward. However, helicopter technology developed so rapidly that some were actually put into use by U.S. troops during World War II.

The helicopter contributed directly to at least one revolutionary production technology. As helicopters grew larger and more powerful, the precision calculations needed for engineering the blades, which had exacting requirements, increased exponentially. In 1947, John C. Parsons of Traverse City, Michigan, began looking for ways to speed the engineering of blades produced by his company. Parsons contacted the International Business Machine Corp. and asked to try one of their new main frame office computers. By 1951, Parsons was experimenting with having the computer's calculations actually guide the machine tool. His ideas were ultimately developed into the computer-numerical-control (CNC) machine tool industry that has revolutionized modern production methods.

William S. Pretzer

Airframe: Preparing the tubing

1 Each individual tubular part is cut by a tube cutting machine that can be quickly set to produce different, precise lengths and specified batch quantities. Tubing requiring angular bends is shaped to the proper angle in a bending machine that utilizes interchangeable tools for different diameters and sizes. For other than minor bends, tubes are filled with molten sodium silicate that hardens and eliminates kinking by causing the tube to bend as a solid bar. The so-called water glass is then removed by placing thebent tube in boiling water, which melts the inner material. Tubing that must be curved to match fuselage contours is fitted over a stretch forming machine, which stretches the metal to a precisely contoured shape. Next, the tubular details are delivered to the machine shop where they are held in clamps so that their ends can be machined to the
required angle and shape. The tubes are then deburred (a process in which any ridges or fins that remain after preliminary machining are ground off) and inspected for cracks.

2 Gussets (reinforcing plates or brackets) and other reinforcing details of metal are machined from plate, angle, or extruded profile stock by routing, shearing, blanking, or sawing. Some critical or complex details may be forged or investment cast. The latter process entails injecting wax or an alloy with a low melting point into a mold or die. When the template has been formed, it is dipped in molten metal as many times as necessary to achieve the thickness desired. When the part has dried, it is heated so that the wax or alloy will melt and can be poured out. Heated to a higher temperature to purify it and placed in a mold box where it is supported by sand, the mold is then ready to shape molten metal into reinforcement parts. After removal and cooling, these parts are then finish-machined by standard methods before being deburred once again.

3 The tubes are chemically cleaned, fitted into a subassembly fixture, and MIG (metal-arc inert gas) welded. In this process, a small electrode wire is fed through a welding torch, and an inert, shielding gas (usually argon or helium) is passed through a nozzle around it; the tubes are joined by the melting of the wire. After welding, the subassembly is stress relieved—heated to a low temperature so that the metal can recover any elasticity it has lost during the shaping process. Finally, the welds are inspected for flaws.

Forming sheet metal details

4 Sheet metal, which makes up other parts of the airframe, is first cut into blanks (pieces cut to predetermined size in preparation for subsequent work) by abrasive water-jet, blanking dies, or routing. Aluminum blanks are heat-treated to anneal them (give them a uniform, strain-free structure that will increase their malleability). The blanks are then refrigerated until they are placed in dies where they will be pressed into the proper shape. After forming, the sheet metal details are aged to full strength and trimmed by routing to final shape and size.

5 Sheet metal parts are cleaned before being assembled by riveting or adhesive bonding. Aluminum parts and welded subassemblies may be anodized (treated to thicken the protective oxide film on the surface of the aluminum), which increases corrosion resistance. All metal parts are chemically cleaned and primer-painted, and most receive finish paint by spraying with epoxy or other durable coating.

Making the cores of composite components

6 Cores, the central parts of the composite components, are made of Nomex (a brand of aramid produced by Du Pont) or aluminum "honeycomb," which is cut to size by bandsaw or reciprocating knife. If necessary, the cores then have their edges trimmed and beveled by a machine tool similar to a pizza cutter or meat slicing blade. The material with which each component is built up from its cores (each component may use multiple cores) is called pre-preg ply. The plies are layers of oriented fibers, usually epoxy or polyimide, that have been impregnated with resin. Following written instructions from the designers, workers create highly contoured skin panels by setting individual plies on bond mold tools and sandwiching cores between additional plies as directed.

7 Completed layups, as the layers of prepreg affixed to the mold are called, are then transported to an autoclave for curing. An autoclave is a machine that laminates plastics by exposing them to pressurized steam, and "curing" is the hardening that occurs as the resin layers "cook" in the autoclave.

8 Visible trim lines are molded into the panels by scribe lines present in the bond mold tools. Excess material around the edges is then removed by bandsawing. Large panels may be trimmed by an abrasive water-jet manipulated by a robot. After inspection, trimmed panels and other composite details are cleaned and painted by normal spray methods. Surfaces must be well sealed by paint to prevent metal corrosion or water absorption.

Making the fuselage

9 Canopies or windscreens and passenger compartment windows are generally made of polycarbonate sheet. Front panels
subject to bird strike or other impact may be laminated of two sheets for greater thickness. All such parts are made by placing an oversized blank on a fixture, heating it, and then forming it to the required curvature by use of air pressure in a freeblowing process. In this method, no tool surface touches the optical surfaces to cause defects.

Installing the engine, transmission,and rotors

10 Modern helicopter engines are turbine rather than piston type and are purchased from an engine supplier. The helicopter manufacturer may purchase or produce the transmission assembly, which transfers power to the rotor assembly. Transmission cases are made of aluminum or magnesium alloy.

11 As with the above, the main and tail rotor assemblies are machined from specially selected high-strength metals but are produced by typical machine shop methods. The rotor blades themselves are machined from composite layup shapes. Main rotor blades may have a sheet metal layer adhesively bonded to protect the leading edges.

Systems and controls

12 Wiring harnesses are produced by laying out the required wires on special boards that serve as templates to define the length and path to connectors. Looms, or knitted protective covers, are placed on the wire bundles, and the purchased connectors are soldered in place by hand. Hydraulic tubing is either hand-cut to length and hand-formed
by craftsmen, or measured, formned, and cut by tube-bending machines. Ends are flared, and tubes are inspected for dimensional accuracy and to ensure that no cracks are present. Hydraulic pumps and actuators, instrumentation, and electrical devices are typically purchased to specification rather than produced by the helicopter manufacturer.

Final assembly

13 Finished and inspected detail airframe parts, including sheet metal, tubular, and machined and welded items, are delivered to subassembly jigs (fixtures that clamp parts being assembled). Central parts are located in each jig, and associated details are either bolted in place or, where rivets are to be used, match-drilled using pneumatically powered drills to drill and ream each rivet hole. For aerodynamic smoothness on sheet metal or composite skin panels, holes are countersunk so that the heads of flat-headed screws won't protrude. All holes are deburred and rivets applied. A sealant is often applied in each rivet hole as the rivet is inserted. For some situations, semi-automated machines may be used for moving from one hole location to the next, drilling, reaming, sealing, and installing the rivets under operator control.

14 After each subassembly is accepted by an inspector, it typically moves to another jig to be further combined with other small subassemblies and details such as brackets. Inspected "top level" subassemblies are then delivered to final assembly jigs, where the overall helicopter structure is integrated.

Upon completion of the structure, the propulsion components are added, and wiring and hydraulics are installed and tested. Canopy, windows, doors, instruments, and interior elements are then added to complete the vehicle. Finish-painting and trimming are completed at appropriate points during this process.

15 After all systems are inspected in final form, along with physical assemblies and appearance aspects, the complete documentation of materials, processes, inspection, and rework effort for each vehicle is checked and filed for reference. The helicopter propulsion system is tested, and the aircraft is flight-tested.

Quality Control

Once tubular components have been formed, they are inspected for cracks. To find defects, workers treat the tubes with a fluorescent liquid penetrant that seeps into cracks and other surface flaws. After wiping off the excess fluid, they dust the coated tube with a fine powder that interacts with the penetrant to render defects visible. After the tubular components have been welded, they are inspected using X-ray and/or fluorescent penetrant methods to discover flaws. Upon completion, the contours of sheet metal details are checked against form templates and hand-worked as required to fit. After they have been autoclaved and trimmed, composite panels are ultrasonically inspected to identify any possible breaks in laminations or gas-filled voids that could lead to structural failure. Prior to installation, both the engine and the transmission subassemblies are carefully inspected, and special test equipment, custom-designed for each application, is used to examine the wiring systems. All of the other components are also tested before assembly, and the completed aircraft is flight-tested in addition to receiving an overall inspection.

The Future

Manufacturing processes and techniques will continue to change in response to the need to reduce costs and the introduction of new materials. Automation may further improve quality (and lower labor costs). Computers will become more important in improving designs, implementing design changes, and reducing the amount of paperwork created, used, and stored for each helicopter built. Furthermore, the use of robots to wind filament, wrap tape, and place fiber will permit fuselage structures to be made of fewer, more integrated pieces. In terms of materials, advanced, high-strength thermoplastic resins promise greater impact resistance and repairability than current thennosets such as epoxy and polyimide. Metallic composites such as aluminum reinforced with boron fiber, or magnesium reinforced with silicon carbide particles, also promise higher strength-to-weight ratios for critical components
such as transmission cases while retaining the heat resistance advantage of metal over organic materials.

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Helicopters

Helicopters. With its ability to hover, take off and land rapidly, and fly close to the world's land and seas, the helicopter has extended the efficacy of air power by bringing it down to earth. In contrast to many other aviation developments which seemed focused on creating an independent role for airpower, for most of its existence helicopter aviation has concentrated on intimate involvement with land and sea forces.

The first complete helicopter (“gyroplane”) performance was accomplished by Louis‐Charles Breguet in 1935. Four years later, Igor Sikorsky captured the imagination of the military with several demonstrations of his VS‐300, XR‐4, and XR‐6 helicopters before high‐ranking officials of various U.S. and British defense units. After developing Sikorsky's ideas, the U.S. military put helicopters into service at the end of World War II, primarily for air rescue. In the Korean War, the United States expanded on tactics developed by the French during their involvement in Algeria, and began experimentally to arm its helicopters. These innovations, along the with deployment of troops by U.S. Marine Corps helicopters, and medical evacuations (medevacs) were key developments in helicopter applications. Helicopters were also used for resupply and observation; and the potential for command and control from above became clearer. The introduction of the helicopter into the battlefield gave the United States a valuable new offensive weapon.

The experiences with helicopters in the Korean War provided impetus for postwar experimentation. Several attempts were made to integrate offensive armaments with other helicopter systems. The U.S. Army, in particular, led by Brig. Gen. Carl I. Hutton, Commandant of the Army Aviation School at Fort Rucker, Alabama, aided by Col. J. D. Vanderpool, sought to construct and employ helicopters which could perform in the traditional cavalry roles, including reconnaissance, flank security, and shock as well as transportation of ground troops.

There was great resistance in political and military circles towards the development of a large, sophisticated, or autonomous army aviation element. One of the main sources of this antipathy was the feeling that all air operations belonged to the air force. Many in the army feared the consequences of a bitter schism similar to that which occurred when the air force itself became autonomous from the army in the previous decade. Proponents, however, argued that army aviation was necessary to fulfill the close air support mission; there was a pervasive feeling, felt most strongly in the army, that the air force was simply not interested in supporting small ground units in close combat.

The development of the UH‐1 “Huey” helicopter gave proponents of an airmobile division the craft, which ultimately persuaded policymakers that such an organization, within the Army, could flourish. Originally planned as an air ambulance, the Huey was later rigged as a gun ship and a troop carrier. The presence of the Huey in all of its multiple roles allowed the army to ask for a division‐sized airmobile unit and to press for the infusion of helicopters into already existing ground units.

Within the army hierarchy individuals such as former paratroop commander Gen. James Gavin were advocates of an increasing role for army aviation. One of Gavin's proteges, Gen. Hamilton Howze, was a Director of Army Aviation and the chief of the Army Tactical Mobility Requirements Board, which during the Kennedy administration advocated an Airmobile Division. Tests for a new 11th Air Assault Division, which largely used UH‐1 Hueys, under Gen. Harry Kinnard began in earnest with a key evaluator being an ardent army aviation supporter, Gen. Robert R. Williams.

In 1965, the army and the air force reached an understanding in which responsibility for helicopter operations were assigned to the army. At approximately the same time the 11th Air Assault Division was redesignated the 1st Cavalry Division (Airmobile), and with its 16,000 troops and more than 400 helicopters was assigned to Vietnam. A second Army division (101st Airborne) became airmobile and aviation assets were assigned to other army and Marine units in large numbers. In many respects the Vietnam War was a “helicopter war” and by 1970 the U.S. Army operated about 12,000 aircraft, the overwhelming majority of which were helicopters.

Helicopters provided American commanders in Vietnam a great deal of flexibility in their operations. They enabled the quick evacuation of wounded troops from the battlefield and saved thousands of lives, thereby holding the politically important death statistics down. Paradoxically, helicopters enabled U.S. troops to engage in combat in areas that otherwise would be inaccessible. The ability to land helicopters in any area with a small cleared space enabled the United States to establish bases known as LZs (landing zones), which produced a battlefield which distinctly lacked a clear demarcation between the friendly and enemy lines. The airmobile capability of helicopters created a more effective fighting force for Vietnam, but it also limited the imagination of tacticians who used this asset in cases where helicopters may not have been the wisest choice to employ. Nevertheless, the sound of helicopters became associated with the Vietnam War in the nightly news and motion pictures.

In 1983, army aviation became a separate branch within the United States army. This was a step along the way toward demand for greater autonomy for army aviators. The Marine Corps organizational structure also promotes considerable autonomy for their aviation forces. Following Vietnam, the army acquired an advanced attack helicopter, the AH‐64 Apache, a modern multi‐purpose craft, the UH‐60 Black Hawk, and an armed reconnaissance craft, the OH‐58D Kiowa Warrior. Other services use, among other helicopters, variants of these craft.

Operation Desert Storm, the American‐led assault to evict Iraqi forces from Kuwait, was initiated in early 1991 by Apache attacks on Iraqi long range radar. The Persian Gulf War presented army aviation with the opportunity to use airmobile tactics to the fullest. The strategic scheme of maneuver for the final assault on Iraqi troops in both Kuwait and Iraq was a flanking attack from the west, known as the “left hook.” The execution of the “left hook,” deep into Iraq, confirmed the faith of military planners who believed in the centrality of helicopters for cavalry and logistical missions.

Over the years the primary criticism of helicopters has been their vulnerability to ground fire. This vulnerability was made clear, once again, when two Black Hawks were shot down in Mogadishu, Somalia almost three years after the Persian Gulf War. Though helicopters may be somewhat vulnerable to ground fire, they are still feared by opposition forces because their ability to fly along the nap of the earth makes them difficult to track via electronic methods. The enemy's frequent inability precisely to locate a helicopter via electronic means contributes to the helicopter's effectiveness and the ground troops' terror. For example, the fear of U.S. helicopters by opposition forces has been noted by implementation force (IFOR) peacekeeping soldiers who served during the Bosnian Crisis in the late 1990s.[See also Rivalry, Interservice; Vietnam War, U.S. Air Operations in.]

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Helicopters

Dictionary of American History
COPYRIGHT 2003 The Gale Group Inc.

HELICOPTERS

HELICOPTERS. Few inventions have changed transportation and military aviation as rapidly and dramatically as the helicopter. The quest for powered flight assumed two forms—horizontal takeoff and vertical take-off—and helicopters and their cousins autogiros, emerged as solutions to the problem of vertical flight. Researchers who pursued vertical flight options sought to capitalize on the increased battlefield surveillance and reconnaissance potential that such craft could provide. Additionally, helicopters promised to offer an inexpensive method of maintaining liaison between central command centers and subordinate units. Experiments with autogiro and helicopter designs occurred throughout Europe, Russia, and the United States from the early 1900s through the interwar years. In 1939, Igor Sikorsky successfully tested his VS 300, the first helicopter with a main rotor that provided lift and a tail rotor that provided directional stability. Sikorsky's solution to the problems of simultaneously lifting and controlling the aircraft launched the helicopter industry in the United States.

Although U.S. forces gained some experience with helicopters late in World War II, the first substantial use of the vertical-takeoff craft came in the Korean War. Between 1950 and 1953, helicopters proved their worth in casualty evacuation, search and rescue, troop insertion, cargo transport, and reconnaissance. In 1950, General Douglas MacArthur requested an increase in the number of helicopters for use as organic aircraft within division, corps, and army headquarters units. U.S. Marine Corps units also used helicopters as organic airlift and combat support assets to bolster tactical combat effectiveness. Perhaps the greatest contribution helicopters made to the war effort in Korea came in the form of aeromedical evacuation. Countless numbers of wounded soldiers owed their survival to dedicated helicopter crews who carried them to field hospitals for emergency medical care. By the end of the Korean War, the U.S. military was committed to developing the helicopter's potential for nearly every conceivable mission.

After the war, helicopter designers concentrated on developing powerful craft that could carry greater payloads over longer distances. Certain industries—oil exploration, for example—came to depend on the economical transportation ability inherent in helicopter technology. The military concentrated on making helicopters an integral

maneuver element of land warfare. The French use of helicopters to patrol and pacify large territories in the Algerian War foreshadowed the U.S. Army's airmobile concepts that came to typify the Vietnam War between 1964 and 1973. Moreover, U.S. army doctrine contained an implicit comparison between lightly armed, mobile guerrilla forces and the mobility that conventional forces obtained using heliborne troops. With this in mind, the army created air cavalry divisions with an assortment of assault, attack, heavy and medium transport, command and control, search and rescue, and medical evacuation helicopters.

The vision of helicopters as organic aviation assets in nearly every army echelon characterized U.S. involvement in the Vietnam War. Army leaders attempted to use helicopters to achieve "vertical envelopments" of Vietcong and North Vietnamese regular forces. According to this concept, ground reconnaissance missions would locate and fix enemy forces until air cavalry units arrived to launch the main American assault. The strategy first emerged in the dramatic Battle of the Ia Drang Valley in 1965, involving the First Cavalry Division (Airmobile) in which U.S. forces engaged and defeated two North Vietnamese army regiments in South Vietnam's central highlands.

Heroic search and rescue crews penetrated heavily defended Vietcong and North Vietnamese positions throughout the war to pluck downed aircrews and wounded soldiers from certain imprisonment or death. Fittingly, the last images of U.S. involvement in Vietnam included helicopters evacuating embassy personnel and refugees from the roof of the U.S. embassy in Saigon (now Ho Chi Minh City) as the South Vietnamese government collapsed in March 1975. In the post-Vietnam era, the U.S. military continued to develop robust helicopter forces. The U.S. Navy in the twenty-first century continued to rely on a wide range of helicopters to support fleet operations in such roles as antisubmarine warfare, troop insertion, countermine operations, search and rescue, and cargo movement. U.S. Air Force special operations units relied on the high-tech Sikorsky MH-53 J/M aircraft, and the U.S. Army developed the Boeing AH Apache Longbow to dominate the combined arms battlefield.

Civilian use of helicopters exploded after the Vietnam War. The same characteristics—speed, mobility, and vertical takeoff and landing—that made helicopters attractive to military forces also appealed to police, emergency services, and firefighting institutions. Law enforcement helicopters from federal to local levels assisted ground units in surveillance and pursuit operations. Emergency service helicopters supported myriad tasks that produced dramatic lifesaving results. Helicopters enhanced firefighting efforts whether in large-scale wildfires or in combating hazardous industrial fires.

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helicopter

The Columbia Encyclopedia, 6th ed.

Copyright The Columbia University Press

helicopter, type of aircraft in which lift is obtained by means of one or more power-driven horizontal propellers called rotors. When the rotor of a helicopter turns it produces reaction torque which tends to make the craft spin also. On most helicopters a small rotor near the tail compensates for this torque. On twin-rotor craft the rotors spin in opposite directions, so their reactions cancel each other. The helicopter is propelled in a given direction by inclining the axis of the main rotor in that direction. The helicopter's speed is limited by the fact that if the blades rotate too fast they will produce compressibility effects on the blade moving forward and stall effects on the rearward–moving blade, at the same time.

The method of flight used by the helicopter was considered by Leonardo da Vinci, in the 16th cent., who described its possibilities but could not provide a propulsion system. Best known among its developers are the French inventor Louis Breguet and the engineers Igor Sikorsky of the United States and Juan de la Cierva of Spain. The helicopter has become very popular for short-distance transportation, because of its maneuverability and ability to land and take off in small areas; it has been adopted for a wide range of services, including air-sea rescue, fire fighting, traffic control, oil platform resupply, and business transportation.

Helicopters have been widely adopted by the military since their first appearance during the Korean War. During the Vietnam War, they became the preferred platforms for transporting troops and evacuating wounded; in the Persian Gulf conflict helicopter gunships provided air cover for advancing tanks. Beginning in early 21st cent. some military helicopters were modified with stealth technology to make them more difficult to track on radar.

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helicopter

hel·i·cop·ter
/ ˈheliˌkäptər/
•
n.
a type of aircraft that derives both lift and propulsion from one or two sets of horizontally revolving overhead rotors. It is capable of moving vertically and horizontally, the direction of motion being controlled by the pitch of the rotor blades. Compare with autogiro.
•
v. [tr.]
transport by helicopter:
the Coast Guard helicoptered a compressor to one ship. ∎ [intr.]
fly somewhere in a helicopter:
the inspection team helicoptered ashore.ORIGIN:late 19th cent.: from French hélicoptère, from Greek helix ‘spiral’ + pteron ‘wing.’

helicopter

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helicopter

helicopterAircraft that gains lift from rotors (rotating aerofoils), and is capable of vertical takeoff and landing, hovering, and forwards, backwards and lateral flight. At take-off, all blades have a steep pitch in order to achieve maximum lift. The circular movement of the blades generates an opposite, reactive force on the helicopter that is overcome by another set of opposite-turning rotors, or by another small rotor in the tail generating thrust in the opposite direction. Igor Sikorsky (1889–1972) built the first successful helicopter in 1939.

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